Describe airfoil, center of pressure, and mean camber line.

Description should include

components of an airfoil
- leading edge
- trailing edge
- chord line
- mean camber line
- maximum thickness
- maximum camber
angle of attack (AOA)
relative wind
cambered airfoil (an asymmetric airfoil for which the mean camber line will be above the chord line)
center of pressure (the moment reference center for which the moment is zero; it depends on the AOA).

PLT236

Process/Skill Questions: